참고문헌 (17)

1. Elverum, G.W., Staudhammer, P. and Miller, J., "The Descent Engine For the Lunar Module," 3rd Propulsion Joint Specialist Conference, Washington, DC., U.S.A., AIAA 1967-521, Jul. 1967. 

2. Gordon, A.D. and Martin, B., "TRW Pintle Engine Heritage and Performance Characteristics," 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2000-3871, Jul. 2000. 

3. Chang, Y., Zou, J., Li, Q. and Cheng, P., "Numerical Study on Combustion and Heat Transfer of a GOX/GCH4 Pintle Injector," 2018 Asia-Pacific International Symposium on Aerospace Technology, Sanghai, China, Jul. 2018. 

4. Muss, A.J., Johnson, W.C., Kruse W. and Cohn K.R., "The Performance of Hydrocarbon Fuels with H 2 O 2 in a Uni-element Combustor," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2003-4623, July. 2003. 

5. Fang, X. and Shen, C.B., "Study on Atomization and Combustion Characteristics of LOX/methane pintle injectors," Acta Astronautica, Vol. 136, pp. 369-379, 2017. 

   상세보기

6. Ryu, H., Yu, I., Kim, W., Shin, D., Ko, Y. and Kim, S., "Experimental Investigation on Combustion Performance of a Pintle Injector Engine with Double-row Rectangular Slot," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 3, pp. 25-33, 2017. 

   원문보기 상세보기

7. Nam, J., Lee, K., Park, S., Huh, H. and Koo, J., "Spray Characteristics of a Movable Pintle Injector with Pintle Tip Shape," The Korean Society for Aeronautical and Space Sciences, Vol. 47, No. 9, pp. 658-664, 2019. 

   원문보기 상세보기

8. Han, D.H., Yoo, Y.L. and Sung, H.G., "An Analysis of the Different Flow Characteristics of a Closed Bomb Test in Cylindrical and Spherical Closed Vessels," International Journal of Aeronautical and Space Sciences, Vol. 20, pp. 150-156, 2018. 

9. Abramzon, B. and Sirignano, W.A., "Droplet Vaporization Model for Spray Combustion Calculations," International Journal of Heat and Mass Transfer, Vol. 32, No. 9, pp. 1605-1618, 1989. 

   상세보기

10. Kang, J.S. and Sung, H.G., "Kerosene/GOx Dynamic Combustion Characteristics in a Mixing Layer Under Supercritical Conditions Using the LES-FP approach," Fuel, Vol. 203, pp. 579-590, 2017. 

    상세보기

11. Shine, S.R., Kumar, S.S. and Suresh, B.N., "A New Generalised Model for Liquid Film Cooling in Rocket Combustion Chambers," International Journal of Heat and Mass Transfer, Vol. 55, pp. 5065-5075, 2012. 

    상세보기

12. Yoo, Y.L. and Sung, H.G., "Numerical Investigation of an Interaction Between Shock Waves and Bubble in a Compressible Multiphase Flow Using a Diffuse Interface Method," International Journal of Heat and mass Transfer, Vol. 127, No. 1, pp. 210-221, 2018. 

    상세보기

13. Zettervall, N., Fureby, C. and Nilsson, E.J.K., "A Small Skeletal Kinetic Mechanism for Kerosene," Energy & Fuels, Vol. 30, No. 11, pp. 9801-9813, 2016. 

    상세보기

14. Strelkova, M.I., Kirillov, I.A., Potapkin, B.V., Safonov, A.A. and Sukhanov, L.P., "Detailed and Reduced Mechanisms of Jet A Combustion at High Temperature," Combustion Science and Technology, Vol. 180, pp. 1788-1802, 2008. 

    상세보기

15. CHEMKIN-PRO 15512, Reaction Design: San Diego, 2011. 

16. Turns, S.R., An Introudction to Combustion Conecpts and Application, 3rd ed., Mc Graw Hill, New York, N.Y., U.S.A., 2012 

17. Morrell, G., "Investigation of Internal Film Cooling of a 1000-pound Thrust Liquid Ammonia Liquid Oxygen Rocket," Technical Report, NACA RME51E04, 1951. 

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